FR2934875B1 - NACELLE OF TURBOREACTEUR MOBILE CHEVRONS. - Google Patents

NACELLE OF TURBOREACTEUR MOBILE CHEVRONS.

Info

Publication number
FR2934875B1
FR2934875B1 FR0804492A FR0804492A FR2934875B1 FR 2934875 B1 FR2934875 B1 FR 2934875B1 FR 0804492 A FR0804492 A FR 0804492A FR 0804492 A FR0804492 A FR 0804492A FR 2934875 B1 FR2934875 B1 FR 2934875B1
Authority
FR
France
Prior art keywords
turboreacteur
chevrons
nacelle
mobile
turboreacteur mobile
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
FR0804492A
Other languages
French (fr)
Other versions
FR2934875A1 (en
Inventor
Pierre Caruel
Martinod Thierry Marin
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Safran Nacelles SAS
Original Assignee
Aircelle SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority to FR0804492A priority Critical patent/FR2934875B1/en
Application filed by Aircelle SA filed Critical Aircelle SA
Priority to RU2011107175/06A priority patent/RU2546347C2/en
Priority to CN200980129622.1A priority patent/CN102105669B/en
Priority to EP09736432A priority patent/EP2321515A1/en
Priority to PCT/FR2009/000980 priority patent/WO2010015751A1/en
Priority to US13/057,935 priority patent/US8430203B2/en
Priority to BRPI0916585A priority patent/BRPI0916585A2/en
Priority to CA2732127A priority patent/CA2732127A1/en
Publication of FR2934875A1 publication Critical patent/FR2934875A1/en
Application granted granted Critical
Publication of FR2934875B1 publication Critical patent/FR2934875B1/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • F02K1/383Introducing air inside the jet with retractable elements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet
    • F02K1/386Introducing air inside the jet mixing devices in the jet pipe, e.g. for mixing primary and secondary flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/46Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing
    • F02K1/48Corrugated nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
FR0804492A 2008-08-06 2008-08-06 NACELLE OF TURBOREACTEUR MOBILE CHEVRONS. Expired - Fee Related FR2934875B1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0804492A FR2934875B1 (en) 2008-08-06 2008-08-06 NACELLE OF TURBOREACTEUR MOBILE CHEVRONS.
CN200980129622.1A CN102105669B (en) 2008-08-06 2009-08-05 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle
EP09736432A EP2321515A1 (en) 2008-08-06 2009-08-05 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle
PCT/FR2009/000980 WO2010015751A1 (en) 2008-08-06 2009-08-05 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle
RU2011107175/06A RU2546347C2 (en) 2008-08-06 2009-08-05 Noise killer for turbojet nacelle equipped with moving herring-bone-like elements and nacelle therewith
US13/057,935 US8430203B2 (en) 2008-08-06 2009-08-05 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle
BRPI0916585A BRPI0916585A2 (en) 2008-08-06 2009-08-05 turbojet nacelle and one-turbojet aero-acoustic noise reduction device
CA2732127A CA2732127A1 (en) 2008-08-06 2009-08-05 Noise reduction device for turbojet nacelle with mobile chevrons, and associated nacelle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0804492A FR2934875B1 (en) 2008-08-06 2008-08-06 NACELLE OF TURBOREACTEUR MOBILE CHEVRONS.

Publications (2)

Publication Number Publication Date
FR2934875A1 FR2934875A1 (en) 2010-02-12
FR2934875B1 true FR2934875B1 (en) 2010-08-13

Family

ID=40430077

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0804492A Expired - Fee Related FR2934875B1 (en) 2008-08-06 2008-08-06 NACELLE OF TURBOREACTEUR MOBILE CHEVRONS.

Country Status (8)

Country Link
US (1) US8430203B2 (en)
EP (1) EP2321515A1 (en)
CN (1) CN102105669B (en)
BR (1) BRPI0916585A2 (en)
CA (1) CA2732127A1 (en)
FR (1) FR2934875B1 (en)
RU (1) RU2546347C2 (en)
WO (1) WO2010015751A1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102010025014B4 (en) * 2010-06-24 2020-10-01 Airbus Defence and Space GmbH Device for reducing jet noise
US8613398B2 (en) * 2011-06-17 2013-12-24 General Electric Company Apparatus and methods for linear actuation of flow altering components of jet engine nozzle
FR2996258B1 (en) * 2012-10-01 2014-10-17 Snecma ALTERNATIVE ROTATION MIXER FOR A TURBOMACHINE CONFLUENT FLUX TUBE AND ITS STEERING PROCESS
FR3008739B1 (en) * 2013-07-18 2017-03-24 Snecma TUYERE OF A TURBOMACHINE EQUIPPED WITH CHEVRONS WITH NON-AXI-SYMMETRIC INTERNAL SIDE.
JP6183837B2 (en) * 2013-08-19 2017-08-23 国立研究開発法人宇宙航空研究開発機構 Exhaust nozzle
US10240560B2 (en) 2014-11-19 2019-03-26 Rohr, Inc. Boot for repair of chevron on nacelle
US10465538B2 (en) * 2014-11-21 2019-11-05 General Electric Company Gas turbine engine with reversible fan
US20170089298A1 (en) * 2015-09-28 2017-03-30 Pratt & Whitney Canada Corp. Deployment mechanism for inflatable surface-increasing features for gas turbine engine
US20170122255A1 (en) * 2015-10-28 2017-05-04 Pratt & Whitney Canada Corp. Chevron system for gas turbine engine
CN112912610B (en) * 2018-09-20 2024-05-17 赛峰飞机发动机公司 Acoustic management on turbines or nacelle
FR3097016B1 (en) * 2019-06-06 2021-07-23 Safran Aircraft Engines CONFLUENCE STRUCTURE OF A PRIMARY VEIN AND A SECONDARY VEIN IN A DOUBLE-FLOW TURBOMACHINE
US12018838B2 (en) 2022-06-21 2024-06-25 General Electric Company Cowl assembly for a gas turbine engine

Family Cites Families (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1422203A (en) * 1964-11-03 1965-12-24 Snecma Improvement in section regulation of silencer effect nozzles
FR1547756A (en) * 1967-10-19 1968-11-29 Snecma Silencers for aeronautical reactors
US3612209A (en) * 1969-11-28 1971-10-12 Gen Electric Propulsion nozzle with combined thrust reverser and sound suppressor mechanism
FR2242568B2 (en) * 1973-08-31 1976-10-01 Snecma
US4279382A (en) * 1980-01-28 1981-07-21 The United States Of America As Represented By The Secretary Of The Air Force Radial and axial flow variable exhaust nozzle for a gas turbine engine
US4754924A (en) * 1987-04-03 1988-07-05 Shannon Aubrey J Variable geometry nozzle
FR2740832B1 (en) * 1995-11-02 1998-01-02 Onera (Off Nat Aerospatiale) DUAL-FLOW TURBOREACTOR BACK
US6220546B1 (en) * 1999-12-29 2001-04-24 The Boeing Company Aircraft engine and associated aircraft engine cowl
GB2372779A (en) * 2001-03-03 2002-09-04 Rolls Royce Plc Gas turbine engine nozzle with noise reducing tabs
US7093423B2 (en) * 2004-01-20 2006-08-22 General Electric Company Methods and apparatus for operating gas turbine engines
FR2868131B1 (en) * 2004-03-25 2006-06-09 Airbus France Sas PRIME TUBE WITH CHEVRONS FOR A DOUBLE FLOW AIRCRAFT AIRCRAFT AND AIRCRAFT COMPRISING SUCH TUYERE
GB0505246D0 (en) * 2005-03-15 2005-04-20 Rolls Royce Plc Engine noise
RU2310766C1 (en) * 2006-02-06 2007-11-20 Открытое акционерное общество "Авиадвигатель" Herringrone reaction nozzle of gas-turbine engine
GB0606823D0 (en) * 2006-04-05 2006-05-17 Rolls Royce Plc Adjustment assembly
GB0608093D0 (en) * 2006-04-25 2006-05-31 Short Brothers Plc Variable area exhaust nozzle
DE102006019299B3 (en) * 2006-04-26 2007-11-08 Deutsches Zentrum für Luft- und Raumfahrt e.V. Aircraft turbofan jet engine, with a primary and a ring-shaped side jet, has an adjustment mechanism of rings to reduce noise emissions on take-off
FR2904372B1 (en) * 2006-07-26 2008-10-31 Snecma Sa GAS EJECTION TUBE FOR DOUBLE FLOW TURBOMACHINE HAVING A VARIABLE EJECTION OR COLLECTION SECTION BY DISPLACING THE SECONDARY HOOD
WO2008045090A1 (en) * 2006-10-12 2008-04-17 United Technologies Corporation Gas turbine engine with rotationally overlapped fan variable area nozzle
US7966826B2 (en) * 2007-02-14 2011-06-28 The Boeing Company Systems and methods for reducing noise from jet engine exhaust
US7883049B2 (en) * 2007-04-27 2011-02-08 The Boeing Company Jet nozzle having noise attenuating shield and method therefor

Also Published As

Publication number Publication date
EP2321515A1 (en) 2011-05-18
RU2011107175A (en) 2012-09-20
US8430203B2 (en) 2013-04-30
BRPI0916585A2 (en) 2015-11-10
CN102105669B (en) 2013-12-25
FR2934875A1 (en) 2010-02-12
US20110139540A1 (en) 2011-06-16
WO2010015751A1 (en) 2010-02-11
CA2732127A1 (en) 2010-02-11
RU2546347C2 (en) 2015-04-10
CN102105669A (en) 2011-06-22

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Legal Events

Date Code Title Description
PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

CD Change of name or company name

Owner name: SAFRAN NACELLES, FR

Effective date: 20180125

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

ST Notification of lapse

Effective date: 20210405